Earlier quoted context omitted.
> "Regenerative cooling" is a rocket term. It came to mind because I used to be an aerospace engineer. There's no requirement in the definition of regenerative cooling for the coolant to be dumped. ? Regenerative cooling in rocketry uses propellant. Propellant is always dumped overboard, because it's propellant. Please show me a rocket that uses closed loop cooling of the rocket nozzle. > Filtering and then compressi…
> Please show me a rocket that uses closed loop cooling of the rocket nozzle The most famous one is the under-development SABRE [1], which includes a closed-loop helium cycle. For cryogenic rockets, closed-loop cooling of the nozzle has been explored [2] to avoid hydrogen embrittlement and oxidation of the nozzle channels, as well as to simplify plumbing. In any case, we've devolved into arguing semantics. > My turn…
From the linked article:
>>The 'hot' helium from the air precooler is recycled by cooling it in a heat exchanger with the liquid hydrogen fuel.
It's open-loop regenerative cooling, with helium as an intermediate coolant. The heat still ends up in the propellant, which gets dumped overboard. Not closed-loop.
That patent also specifies a heat exchanger to the propellant tank.
>I was figuring on dumping the air once done versus worrying about a reservoir.
A poorly telegraphed joke. The atmosphere, here, is the reservoir. I have edited my comment.